What was found
FUSELAGE SKIN PANEL CRACKED BETWEEN BS 827+5. TO 827+5.5, STRINGER 17L. REPAIRED SKIN IAW SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN PANEL CRACKED BETWEEN BS 827+5. TO 827+5.5, STRINGER 17L. REPAIRED SKIN IAW SRM.